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Accidents · NTSB DCA15CA117 · Final report

Titan Aerospace Holdings INC SOLARA 50 accident near Otto, New Mexico, May 1, 2015

On May 1, 2015 at about 5:07 pm local time, a 2014 Titan Aerospace Holdings INC SOLARA 50, registered N950TA, was destroyed in an accident during initial climb near Otto, New Mexico (Private Aerodrome airport). It was a flight test under general aviation rules (Part 91). No one was hurt. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

structural failure of the left wing due to an overspeed condition.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
May 1, 2015 · about 5:07 pm local time
Place
Otto, New Mexico · Private Aerodrome · map
Type
Accident
Injuries
No one was hurt.
Weather
visual conditions (good weather)
Aircraft
Titan Aerospace Holdings INC SOLARA 50 NO SERIES, built 2014
Registration
N950TA · no longer on the register · serial 0001
Damage
Destroyed
Flight
Flight test · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

On May 1, 2015 at 11:07 Mountain Daylight Time (MDT), a Titan Solara 50 solar-powered unmanned experimental aircraft registration N950TA crashed shortly after takeoff, near Otto, New Mexico.  The aircraft was operated as a scaled, proof of concept test flight.  The aircraft was destroyed, there were no injuries. According to the operator, at 11:02:43 the aircraft began a controlled winch tow and rolled on the ground until liftoff.  After the tow release at approximately 30 ft above ground level (AGL), the pilot transitioned to flying the aircraft via instruments and the aircraft was powered up to full throttle for a straight ahead climb.  The pilot immediately recognized that the instruments were exhibiting complicating latency and focused on flying the aircraft to a safe altitude and position where the external pilot (copilot) could take control and visually land the aircraft. The pilot initiated a left hand turn when the aircraft reached approximately 160 feet AGL, which continued until the aircraft reached approximately 385 feet AGL.   During this time the pilot made two power reductions, attempting to stabilize the aircraft at an altitude and heading acceptable for handover to the copilot to conduct an external visual landing.  Handover of controls to the copilot was not attempted during the flight. The operator indicated that the aircraft then encountered significant thermal air mass activity and began to both climb and exceed its design airspeed for an extended period of time.  Visible deformation of the wing structure was witnessed by ground personnel during the overspeed condition.  It achieved a maximum altitude of approximately 520 feet AGL just prior to structural failure of the left outboard wing.  These thermal events were not immediately evident to the pilot due to latency of the aircraft instruments.  It is believed the subsequent wing deformation caused the aircraft to begin an uncontrollable right hand turn that the pilot was unable to arrest. Coincident with the significant wing deformation, the aircraft began an uncontrollable and erratic flight path roughly straight ahead in a rapid descent.  The left outboard wing section separated from the aircraft during the first portion of the descent and the right outboard wing section separated later in the descent.  The aircraft impacted the ground at 11:06:59 with the majority of the structure intact and in a nose down attitude.  There were no meteorological indicators that clearly showed evidence of significant pre-launch thermal activity in the test flight area. The aircraft was destroyed when it struck the ground in a rural unpopulated area.  Local terrain surrounding the takeoff area, intended landing area (same as takeoff location), and accident site consisted of flat desert grassland.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Aircraft structural failure during initial climb defining event

The NTSB's findings

  • cause Aircraft › Aircraft structures › Wing structure › Spar (on wing) › Failure
  • factor Environmental issues › Conditions/weather/phenomena › Turbulence › (general) › Ability to respond/compensate

Pilot

  • Certificate: airline transport pilot, flight instructor, commercial pilot, flight engineer
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane; rotorcraft: glider
  • Flight time: 6,000 hours in all; 1 in this make and model; 13 in the last 90 days; 8 in the last 30 days; 2,400 as pilot in command; 375 on instruments
  • Last flight review: June 12, 2014
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

Co-pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 296 hours in all; 1 in this make and model; 0 in the last 90 days; 250 as pilot in command; 0 on instruments
  • Last flight review: March 31, 2014
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 0.1 hours
  • Last inspection: condition inspection, April 27, 2015; 0 hours since
  • Maximum gross weight: 350 lb
  • Seats: 0
  • Landing gear: fixed
  • Engine: Ramazani & Assoc. M19 (electric); 0 hours total
  • Operator: Titan Aerospace Holdings INC

The flight

  • Departed from: NA Otto NM at 5:02 pm
  • Destination: NA Otto NM
  • Flight plan: VFR

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: a few clouds
  • Temperature: 72°F (22°C), dew point 27°F (-3°C)
  • Altimeter: 30.18 inHg
  • Observation at 5:00 pm from 0E0, 1 miles away

Documents from the investigation the NTSB's docket: the evidence folder behind the report

1 document, released by the NTSB on November 19, 2015. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.